N14381
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
17 reports on file, 1995-11-08 – 2001-01-17.
Part: DOOR — GOUGED (LT NLG) · airframe 18,678 hrs · 9,973 cycles
INSPECTION FOUND LT NOSE GEAR DOOR GOUGED AT I/B EDGE JUST AFT OF FORWARD END. THE FILLER AND RETAINER AT NOSE GEAR DOOR WERE REMOVED AND REPLACED IAW SRM 51-10-02.
Part: SKIN — GOUGED (LT WING) · airframe 18,678 hrs · 9,973 cycles
INSPECTION FOUND LT WING LOWER SKIN GOUGED AFT I/B T/E AT WING ROOT JUST FORWARD OF GEAR BAY. A REPAIR WAS INSTALLED IAW SRM 51-40-02.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 18,678 hrs · 9,973 cycles
INSPECTION FOUND A 2 INCH CRACK IN ANGLE AT STA 727, RBL 12. A REPAIR WAS INSTALLED IAW SRM 51-70-11.
Part: STRAP — GOUGED (HORIZONTAL STAB) · airframe 18,678 hrs · 9,973 cycles
INSPECTION FOUND BOWTIE STRAP GOUGED AT TAIL CONE ATTACH POINT AFT OF RT HORIZONTAL STABILIZER ATTACH FITTING. REPLACED WITH NEW STRAP IAW SRM 51-10-2.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 18,678 hrs · 9,973 cycles
INSPECTION FOUND FLOORBEAM CAP CORRODED AT STA 986, LBL 6 TO LBL 24. A REPAIR WAS INSTALLED IAW SRM 53-00-51, FIGURE 203.
Part: WEB — TORN (FUSELAGE) · airframe 18,678 hrs · 9,973 cycles
INSPECTION FOUND WEB EDGES TORN AWAY AT AFT CARGO DOOR OPENING, FORWARD LOWER INTERNAL FACE OF JAMB, STA 809. THE DAMAGED WEB WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 51-70-13.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 18,678 hrs · 9,973 cycles
INSPECTION FOUND A 1 INCH CRACK IN FORWARD BAGGAGE BIN ANGLE BRACKET AT STA 380, S26R. THE ANGLE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-02.
Part: FLAP TRACK — GOUGED (NR 3 TE FLAPS) · airframe 18,678 hrs · 9,973 cycles
INSPECTION FOUND NR 3 AFT FLAP NR 2 TRACK FROM I/B ON RIGHT WING GOUGED. THE FLAP TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW MM 57-53-18.
Part: FRAME — CRACKED (FUSELAGE) · airframe 18,678 hrs · 9,973 cycles
INSPECTION FOUND A .5 INCH CRACK AT RIVET HOLE IN FRAME AT STA 360, S8L. THE FRAME WAS REPAIRED IAW SRM 53-00-07, FIGURE 201.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 18,678 hrs · 9,973 cycles
INSPECTION FOUND FLOORBEAM CORRODED AROUND FASTENER HOLES FROM ENTRY DOOR TO SERVICE DOOR, STA 312, RBL 21 TO LBL 38. A REPAIR FLOORBEAM WAS INSTALLED IAW SRM 53-10-51, FIGURE 205.
Part: FLAP TRACK — GOUGED (NR 2 TE FLAPS) · airframe 18,678 hrs · 9,973 cycles
INSPECTION FOUND NR 1 MIDFLAP, NR 2 AFT FLAP TRACK AFT SECTION GOUGED. THE FLAP TRACK WAS REMOVED AND REPLACED IAW MM 57-53-18.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 18,678 hrs · 9,973 cycles
INSPECTION FOUND Z-ANGLE CORRODED AT STA 1000, RBL 35. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 18,678 hrs · 9,973 cycles
INSPECTION FOUND FLOORBEAM CAP CORRODED AT STA 344, LBL 25. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-51, FIGURE 203.
Earlier reports · 1995–2000 · 4 reports
2000
Part: CHANNEL — CORRODED (FUSELAGE) · airframe 17,330 hrs · 9,280 cycles
INSPECTION FOUND TWO CHANNELS CORRODED IN AFT CARGO COMPARTMENT ON LT AND RT SIDES AT STA 727 - 849. THE CHANNELS WERE REPAIRED IAW SRM 53-60-53, FIGURE 204.
1999
Part: WIRE — BROKEN (ROW 18)
INSPECTION FOUND EMERGENCY LIGHT INOPERATIVE AT SEAT ROW 18 ABC. MAINTENANCE FOUND CONNECTOR END PULLED FROM HARNESS. REMOVED AND REPLACED WIRE ASSEMBLY AND OPERATION CHECKED GOOD.
1996
Part: WIRE — BROKEN (CABIN)
FLT NR 1979 - EWR - INSPECTION FOUND ALL EMERGENCY AISLE PATH LIGHTS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AND PIN PULLED OUT OF PLUG AT ROW 11. THE PIN WAS REINSTALLED AND THE WIRE WAS REPAIRED. IN ADDITION, A BLOWN BATTERY PACK FUSE WAS REPLACED. OPERATIONAL CHECKS WERE GOOD. (M)
1995
Part: FUSE — FAILED (CABIN)
CLE - FLT 1549 - THE LT OVERWING INTERIOR EXIT LIGHT FAILED TO ILLUMINATE ON TEST. MAINTENANCE FOUND A BAD FUSE IN THE BATTERY PACK. THE FUSE WAS REPLACED AND OPERATION OF THE EXIT LIGHT WAS RESTORED. (X)